Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.
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THERMAL INSULATING SLEEVE LINER FOR FLUID FLOW DEVICE AND
FLUID FLOW DEVICE INCORPORATING SUCH LINER
CROSS-REFERENCES TO RELATED APPLICATIONS
[0001] This application claims the benefit of U.S. Provisional Patent
Application
No. 62/823,357, filed March 25, 2019, the entire content of which is herein
incorporated by reference.
STATEMENT REGARDING FEDERALLY
SPONSORED RESEARCH OR DEVELOPMENT
[0002] (NOT APPLICABLE)
BACKGROUND & SUMMARY
[0003] Fluid flow devices (e.g., pipes, valves, nozzles and the like)
subjected to
thermal shocks in severe industrial applications can benefit from thermal
protection to
reduce thermal stresses, mitigate the effects of thermal shock experienced and
prevent
premature thermal fatigue. Fluid flow devices subject to cyclic high pressure
and
temperature changes make them prone to failure due to thermal shock. Thermal
shock
refers to a process wherein the flow device experiences sudden large magnitude
changes in thermal stress when the heat flux and temperature gradient
experienced by
the flow device change abruptly.
[0004] Thermal shock damage can be found in various severe service
industries
(e.g., in a catalyst injection valve and its connection pipes in an ebullated
bed hydro-
processing ore refining application). In the case of an ebullated bed hydro-
processing
system, for instance, cracking of valve body and metal valve seats has been
observed
when valves are exposed to temperatures and pressures of up to 850 F and
3,150 psi at
4-10 cycles per day. Cracking is thought to occur due to initial thermal
stresses
experienced when the valve is opened to experience such high temperature and
pressure
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after several hours of having remained closed and therefore having reached
ambient
temperature. This phenomenon is especially observed during winter when
external
ambient temperature drops (e.g., to as low as -40 F) and pre-heating systems
fail.
[0005] Over the years, several innovations have been presented to help
mitigate
the effects of temperature surges and, in some cases, proposed solutions have
been
adopted. Some of the attempted solutions currently in use include use of
materials
having low thermal conductivity, use of pre-heating systems, use of thermal
barrier
coatings which are highly refractive, etc. While these attempted solutions
have
achieved some level of success, they continue to present shortcomings which
are here
addressed by several example embodiments of improved thermal insulating sleeve
liners for fluid flow devices used in severe industrial applications.
[0006] Pre-heating systems have proven to be unreliable. There are
reported
cases where pre-heating systems malfunctioned and resulted in valve operations
being
carried out without pre-heating. Cracking of the valve body is especially
observed
when this occurs, and regular maintenance is required to avoid such incidents.
This
may be costly but even then normal operation is not guaranteed, especially
during harsh
weather conditions.
[0007] Adoption of low thermal conductivity materials has been proven not
as
effective since cracking could still be observed on the bodies of flow
devices. This is a
clear indication of their susceptibility to extreme cyclic temperatures. This
led to the
adoption of thermal barrier coatings (TBCs). While TBCs have generally been
more
effective in providing thermal shock protection, they too have several
limitations.
TBCs are susceptible to erosion and corrosion, especially in instances where
they are in
the flow path. TBCs require laborious and expensive processes for their
preparation
which results in high initial costs. And TBCs are notoriously brittle and
prone to
corrosion and erosion. Sleeves with TBCs need to be frequently replaced.
[0008] Some non-exhaustive examples of prior thermally insulating sleeve
liners
or other thermally protective internal interfaces for fluid flow devices can
be found, for
example, in the following prior published US patent documents: Newberg US
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7,017,602; Williams, Jr., et al. US 8,783,279; Hofmann US 2018/0051834; and
Zhu et
al. US 2018/0209322.
[0009] The present document describes an improved, preferably additively
manufactured (e.g., by 3D printing), thermal insulating sleeve liner
constructed of a
suitable material for the serviced application (e.g., Inconel 718 or other
austenitic
nickel-chromium-based super-alloys, high nickel alloys and the like or ceramic
and/or
composite materials of various types recognized by those in the art as being
suitable for
certain severe service applications) with an internal infill structural
pattern creating
internal voids which increase thermal insulation properties while yet
remaining
structurally adequate to serve as a thermal insulating flow device liner for
the serviced
application. Preferably the infill is sized to maximize strength (i.e., to
support
internal/external pressures to be experienced by the sleeve) while
concurrently also
minimizing heat transfer (i.e., from the inside to the outside of the sleeve).
Multi-layer
material could also be used if the sleeve is made with wear-resistant,
corrosion-
resistant, low thermal conductivity materials. When a 3D printed sleeve comes
out of
the printer, it is in a green state. Subsequently parts can be subjected to
hot isostatic
pressing (sometimes referred to as being "hipped") and/or heat treated to
reduce
porosity and increase mechanical properties respectively. Based on testing,
all these
three states are believed to work.
[0010] An object of example embodiments described herein is to provide a
thermal protection device with varying designs based on the method of
manufacture
and intended application.
[0011] In one example embodiment, an additively manufactured (i.e., 3D
printed) thermal sleeve includes two spaced-apart cylindrical shells and an
internal
infill pattern of integrally-formed supporting structure there-between. This
thermally
insulating sleeve is fitted into the flow path of the protected flow device
(e.g., valves,
pipes and the like). The sleeve could be locked by an interference fit with
the body.
Other locking methods such as brazing, welding or one or more retaining rings
could be
considered as well. The infill may have variable patterns that may be in the
form of,
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but not limited to, centroidally-directed lattices, hollow honeycomb-like
structures and
so forth. These patterns form a porous network of supporting structure
containing voids
between the two shells. This network of structure entraps air (or other
insulating
material such as an inert nitrogen gas or an insulating vacuum) thus allowing
for heavy
internal insulation of flow devices to prevent or reduce thermal shock
therein.
Tessellations or other structural patterns inside the sleeve allow for free
design of infill
percentage making it customizable depending on process requirements and
parameters.
The end of the sleeve may be left open or fused. For sleeves having fused
ends, the air-
tight infill patterned region or chamber can be vacuumed or pressurized (e.g.,
with air
or an inert gas).
[0012] In another example embodiment, a pressure equilibrium hole can be
made
on or through the sleeve. While the sleeve can remain acting as if a solid air-
tight
structure, the pressure equilibrium hole ensures a pressure balance between
its inner
and outer surfaces.
[0013] In another example embodiment, a non-encapsulated thermal sleeve
is
slip-fitted into a flow device bore. This sleeve can have variable exterior
protruding
surface patterns which can change depending on process requirements. Examples
of
these may include axially ribbed or radially ribbed exterior protruding
surface patterns.
Exterior surface patterns reduce the surface area in thermal contact with the
interior
bore body of the flow device while still allowing air entrapment there-within.
This
device is preferably additively manufactured (e.g., by 3D printing) although
some
embodiments may be manufactured by other processes. Depending on the
application,
the thermal sleeve may have a wear and abrasion resistant layer on its inner
surface.
Such functional graded layers can be deposited either by conventional
deposition
methods (such as a spray of thermal material) or by additive manufacturing
(i.e., 3D
printing) processes.
[0014] For an example embodiment installed in a flow device, the
different
sleeve concepts may be capped (e.g., using a separate circumferential ring-
shaped cap
structure) or they may have an integrally-formed circumferential ring-shaped
lip in
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other embodiments to secure and/or locate the sleeve within the flow device.
The
lipped sleeve may be produced as a single piece while the capped sleeve has
two
distinct parts: the main sleeve part and the securing cap part. The lip or cap
can interact
with a larger diameter bore section at a proximal end of the main sleeve part
and a
narrower diameter bore section at the other distal end of the main sleeve part
(so as to
locate and trap the main sleeve part at a desired location within the flow
device bore).
The cap may be of the same material as the sleeve or of the same or similar
material as
the flow device. The securing cap can be welded to the flow device on the
proximal
larger diameter bore section after the main sleeve part has been snug-fit into
a main
bore length against the end face of a smaller diameter distal bore section
thus retaining
the main sleeve part at a desired location. The lip of a lipped sleeve, if
that is used
instead of a separate cap ring, can be similarly welded directly to the body
of the flow
device at the larger diameter proximal bore section to retain the sleeve at a
desired
location.
[0015] Some example embodiments of an improved additively manufactured
thermal insulating sleeve liner are sized to have an outside dimension and
surface area
purposefully smaller than the inside dimension and surface area of the
protected flow
device, thereby reducing sleeve liner thermal contact with the protected flow
device and
thus enhancing its thermal protection. Dimensions should provide the loosest
possible
fit so long as it does not permit or cause excessive vibration or permit
ingress of
thermally conductive material in use. In some embodiments, a loose fit
clearance of a
few thousands of an inch (e.g., on the order of 0.002 inch) may be suitable.
[0016] Some example embodiments of the improved additively manufactured
thermal insulating sleeve liner may include spaced-apart external (i.e.,
outwardly
protruding) structures to insure less thermal contact with the internal
surface of a
protected flow device thus further reducing sleeve liner thermal contact with
the
protected flow device and enhancing its thermal protection.
[0017] Some example embodiments of the improved additively manufactured
thermal insulating sleeve liner may include an integrally formed larger
diameter lip at
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one end to assist in locating and/or retaining the sleeve liner properly
within the
protected flow device. Such a locating/retaining end lip (e.g., a diameter
larger than the
main sleeve liner body to retain a respectively associated end at a proper
location in
use) may also be formed as a separate retaining cap-ring structure that is
secured (e.g.,
by a few tack or seal welds) at a proper location within the protected flow
device.
[0018] Some example embodiments of the improved additively manufactured
thermal insulating sleeve liner are installed within a protected flow device
so as to
provide an integrated flow device product incorporating the improved thermal
insulating sleeve. However in use, due to wear and/or other deterioration in
use, it will
likely be necessary to periodically remove the thermal insulating sleeve
(e.g., by
breaking spot or seal welds holding it in place) and replace it with a new or
refurbished
thermal insulating sleeve. And if a flow device is not initially provided with
the
improved additively manufactured thermal insulating sleeve, then one can be
retro-
fitted into the flow device to thereafter provide desired thermal protection.
[0019] The improved additively manufactured thermal insulating sleeve
liner is
preferably constructed so as to prevent ingress of thermally conductive
materials (e.g.,
catalyst particles which may typically be on the order of 0.8¨ 1.0 mm in
diameter with
nickel-molybdenum active metal catalysts) into internal voids of the
insulating sleeve
or between the outer sleeve surface and the internal surface of the protected
flow
device. In this way the thermal insulating and protective properties of the
sleeve can be
better maintained. At the same time, some pressure equalization may be needed,
at
least in some applications, between the inside and outside surfaces of the
insulating
sleeve (perhaps including internal voids of the sleeve). If a pressure
equalization path
is needed, care should be taken to keep the pressure equalization path(s)
small enough
to prevent ingress of flowing thermally conductive particles (e.g., metallic
catalyst
particles).
[0020] Some example embodiments of the additively manufactured thermal
insulating sleeve liner have two solid shells sandwiching a concurrently
formed
additively manufactured infill pattern (i.e., manufactured by a conventional
3D printing
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process). The infill pattern may vary and may range from simple honeycomb
structures
to complex lattice structures depending on process requirements and
parameters. The
sleeve may have an open end, or the ends may be fused to make the sleeve
airtight. In
the case of an airtight sleeve, the infill pattern chamber voids may be
vacuumed or
pressurized.
[0021] Some example embodiments of the additively manufactured thermal
insulating sleeve liner are non-encapsulated with variable patterns on the
external
sleeve surface that may be modified depending on the application.
[0022] Some example embodiments of the additively manufactured thermal
insulating sleeve liner have a wear-resistant coating along the axial flow
way.
[0023] Some example embodiments of the additively manufactured thermal
insulating sleeve liner are trapped via a separate retaining cap or have an
integral lip
which in either case is welded to one end of the bore to be protected on the
flow device
(e.g., with spot welds or seal welds that can be easily broken when it is
desired to
remove/replace a previously installed insulating sleeve).
[0024] The example embodiments described herein offer several advantages.
The additively manufactured (e.g., 3D printed) thermal insulating sleeve
device is
produced in one manufacturing step resulting in considerable savings. It
requires little
lead time as the design process is much shorter than other manufacturing
methods.
Validation of the parts can commence as soon as the part is printed. Since the
device
can be additively manufactured, unique and more complex structures can be made
for
the infill without interfering with sleeve integrity. Additionally, there is
very little
material wasted in an additive manufacturing process and a homogeneous density
of the
resulting insulating sleeve ensures a more evenly distributed sleeve strength.
[0025] To reduce the laborious procedure that would involve dis-assembly
of the
protected flow device during part replacement or planned plant maintenance,
the
present example embodiments are designed to be easily replaceable upon
reaching the
end of design life. This can be done by removing the flow device from the
process and
sliding the loosely fit sleeve out of the flow device bore (after light
holding spot or seal
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welds are broken). Additionally, toughness of the material involved will
ensure that the
sleeve is more robust than in the past thus ensuring, among other things, less
scrap and
a potential for the sleeve material to be re-used.
BRIEF DESCRIPTION OF THE DRAWINGS
[0026] The accompanying drawings depict various example embodiments for
illustrative purposes but are not to be construed as limiting the scope of
later appended
claims.
[0027] FIG. 1A is an isometric view of an example additively manufactured
open-ended thermal insulating sleeve with an accompanying enlarged local
section at
FIG. 1A-1 to better depict an infill pattern sandwiched between two shells;
[0028] FIG. 1B is an isometric view of an example additively manufactured
fuse-
ended thermal insulating sleeve with an accompanying enlarged local section at
FIG.
1B-1 to better depict the internal infill pattern as in FIG. 1A-1;
[0029] FIG. 2A is an isometric view of an example additively manufactured
capped (or lipped) at one end and open-ended at the other end thermal
insulating sleeve
with an accompanying enlarged local section at FIG. 2A-1 to better depict an
infill
pattern sandwiched between two shells;
[0030] FIG. 2B is an isometric view of an example additively manufactured
capped (or lipped) at one end and fused at the other end thermal insulating
sleeve with
an accompanying enlarged local section at FIG. 2B-1 to better depict the
internal infill
pattern as in FIG. 2A-1;
[0031] FIG. 3A is an isometric and partially sectioned view of an example
capped and additively manufactured radially ribbed thermal insulating sleeve;
[0032] FIG. 3B is an isometric and partially sectioned view of an example
lipped
and additively manufactured axially ribbed thermal insulating sleeve;
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[0033] FIG. 4 is a schematic sectioned isometric view of an example
capped
thermal protection sleeve installed in a flanged flow device with an enlarged
local
section at FIG. 4A to better depict the internal infill pattern;
[0034] FIG. 5 is a schematic partially sectioned view of an example
lipped
thermal protection sleeve installed in a bore on a protected flow device and
an
accompanying enlarged partial sectional view at FIG. 5-1 to better illustrate
how it is
fitted into the bore;
[0035] FIG. 6 is a schematic partially sectioned view of an example
capped
thermal protection sleeve installed in the bores of a flow device and an
accompanying
enlarged partial sectional view at FIG. 6-1 to better illustrate how a capped
sleeve is
fitted into a bore; and
[0036] FIG. 7 is a schematic partially sectioned isometric view of a
valve flow
device having two flanged end connection pipes with installed thermal
protection
sleeves there-within.
DETAILED DESCRIPTION OF EXAMPLE NON-LIMITING EMBODIMENTS
[0037] In the accompanying drawings identical reference numerals may have
been used to identify features which are identical or similar in function. The
example
embodiments demonstrate varied designs based on similar concepts to provide an
overall view of example thermal insulating sleeve liner interactions with flow
devices.
[0038] FIG. 1A is a schematic isometric general overview of a thermal
insulating
sleeve 10 having an inner shell 12, outer shell 14, an infill pattern 16 of
supporting
structure with included voids provided between the inner and outer shells 12,
14, and
open ends 18 (e.g., see FIG. 1A-1). The material and infill pattern 16 of the
thermal
sleeve can be varied to offer different strengths and thermal insulation
depending on the
application for which it is intended. As those in the art will appreciate, a
typical
ebullated bed hydro-processing application flow device conveys a corrosive
liquid
carrying small (e.g., 0.8 ¨ 1.0 mm diameter) titanium catalyst particles at
temperatures
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on the order of 800¨ 1,100 F at a pressure on the order of 3,400 psi. In this
application, as those in the art will appreciate, a thermal insulating sleeve
liner could
typically be made of a tungsten alloy. As those in the art will recognize, the
material
and structure of the thermal insulating sleeve liner must be chosen
appropriately in
accordance with conventional standard design practices to accommodate process
parameters of the application being serviced. Such sleeve characteristics are
typically
determined by the extreme pressures and temperatures to which the sleeve will
be
subjected. The thermally insulating sleeve liner 10 can be slip-fit into a
flow device
bore. The open ends 18 should be fitted to mating internal surfaces of the
flow device
sufficiently closely to make it impossible for solid entrapment (e.g., of
metallic
thermally conductive catalyst particles) within the chamber of the infill
pattern 16 or
between the outer shell 14 and the inner surfaces of the flow device.
[0039] Complex lattice infill patterns 16 provide a longer and indirect
path for
thermal conduction while air (or other insulating material or vacuum) trapped
in
between the two shells due to interstices of the infill pattern 16 possesses
poor thermal
conduction properties leading to increased thermal insulation.
[0040] FIG. 1B is a schematic isometric general overview of a thermal
insulating
sleeve 20 having an inner shell 12, outer shell 14, an infill pattern 16 of
supporting
structure with included interstice voids provided between the inner and outer
shells 12,
14, and fused ends 22 (i.e., closed ends 22 as depicted in FIG. 1B-1 so as to
encapsulate
the voids included within the infill structure 16 between shells 12, 14 and
ends 22). As
with the thermal sleeve 10 of FIGs. 1A and 1A-1, the material and infill
pattern 16 of
the thermal sleeve 20 can be varied to offer different strengths and thermal
insulation
depending on the application for which it is intended. Here the voids within
the
chamber containing infill pattern 16 can be vacuumed or pressurized before
ends 22 are
fused shut (e.g., one end can be left partially open and connected to a source
of vacuum
or pressurized thermally insulating gas or liquid fluid before this partial
opening is also
fused to a fully closed configuration). Once the voids are thus suitably
treated and the
ends 22 fused to a closed state, the thermally insulating sleeve liner 20 can
be slip-fit
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into a flow device bore. The fused closed ends 22 make it impossible for solid
entrapment (e.g., of metallic thermally conductive catalyst particles) within
the
chamber of the infill pattern 16. The fused ends 22 should be fitted to mating
internal
surfaces of the flow device sufficiently closely to make it impossible for
solid
entrapment (e.g., of metallic thermally conductive catalyst particles) between
the outer
shell 14 and the inner surfaces of the flow device.
[0041] While some prior art thermally insulating sleeve liners have been
shrink-
fitted into tight engagement with the internal walls of the flow device, it is
preferred to
only loosely slip-fit the thermally insulating sleeve liner 10 or 20 within
the internal
bore walls of the flow device so as to provide additional thermal insulation
between a
hot corrosive high pressure flowing substance and the flow device structures.
[0042] FIG. 2A and FIG. 2B depict the example thermal insulating sleeves
10
and 20, respectively, with an included securing cap or lip 24 at one end. A
securing cap
may be separately constructed and fitted at an end of the sleeve when
installed within a
flow device to secure it at a proper location in use within a flow device. A
securing lip
may be constructed as an integral part of the sleeve at an end to secure it at
a proper
location in use within a flow device.
[0043] FIG. 3A depicts an example capped radially-ribbed thermally
insulating
sleeve liner 30. The externally extending interstices between ribs 32 will
provide
additional thermally insulating spaces when fitted within the internal
surfaces of a flow
device bore. Example sleeve liner 30 is preferably created by additive
manufacturing
(i.e., 3D printing) to provide a central portion of the sleeve body between
inner and
outer shells with an infill pattern as in the examples of FIGs. 1A, 1A-1, 1B,
1B-1, 2A,
2A-1, 2B, and 2B-1 to provide still further thermal insulation as in these
earlier-
described embodiments. The section cut highlights an end contact between the
sleeve
30 and a separate securing cap 34 (which functions, like the securing cap of
earlier-
described embodiments). As those in the art will recognize, the securing cap
34 could
be replaced by an integrally manufactured securing/locating lip if desired (as
depicted
in FIG. 3B).
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[0044] FIG. 3B depicts an example lipped axially-ribbed thermally
insulating
sleeve liner 36. The externally extending interstices between ribs 38 provide
thermally
insulating spaces when fitted within the internal surfaces of a flow device
bore.
Example sleeve liner 36 is preferably created by additive manufacturing (i.e.,
3D
printing) to provide a central portion of the sleeve body between inner and
outer shells
with an infill pattern as in the examples of FIGs. 1A, 1A-1, 1B, 1B-1, 2A, 2A-
1, 2B,
2B-1 to provide still further thermal insulation as in these earlier-described
embodiments. The section cut highlights the integrally formed
securing/locating lip 40
formed at an end of the sleeve 36 (which functions, like the locating/securing
lip of
earlier-described embodiments). As those in the art will recognize, the
locating/securing lip 40 could be replaced by a separate securing/locating cap
if desired
(as depicted in FIG. 3A).
[0045] When disposed about an axial flow passage within a flow device
bore
(e.g., as shown in FIGs. 4-7), the externally ribbed sleeve 30 or 36 makes
less surface
contact with the flow device bores due to the surface pattern of ribs on its
exterior
thereby reducing thermal stress concentration points.
[0046] While FIGs. 3A and 3B illustrate two options of radially-ribbed
and
axially ribbed exterior surfaces, as those in the art will appreciate, the
ribbed pattern can
be modified as desired to accommodate requirements of various processes.
[0047] FIGs. 4 and 4-1 depict a capped thermal protection sleeve 42
installed in a
flow device 44. The thermally insulating sleeve 42 (of any example embodiment
described herein) can be disposed in a flow device (e.g., flanged pipe 44)
detachably
connectable to other flow devices (e.g., valves). The interaction between the
sleeve 42
and the pipe 44 is like that between an example sleeve and the internal flow
surfaces of
other flow devices (e.g., valves). The example thermally insulating sleeve 42
is slip-
fitted into a bore of the pipe body that has a smaller diameter end portion
locating and
closing (if the sleeve does not already have a closed end) one end of the
sleeve 42 to the
ingress of flowing thermally conducting materials in use. A securing cap 46,
disposed
within a larger diameter end portion of the flow device bore, secures and
locates the
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other end of the thermal insulating sleeve 42 within the flow device bore (and
closes it
to ingress of flowing thermally conducting materials in use if the sleeve does
not
already have a closed end).
[0048] FIG. 5 depicts lipped thermal protective sleeves 50, 52 slip
fitted into
flanged pipe input/output ports of a valve 54. In an enlarged partial section
view
depicted at FIG. 5-1, the outer surfaces of integral securing/locating lip 56
of sleeve 52
is mated to a larger diameter proximal internal bore section 58 while the main
body of
sleeve 52 is slip-fit into the relatively narrower main bore 60 of the flow
device valve
54 ¨ and the other end of sleeve 52 is butted to a narrower diameter distal
bore section.
The lip 58 is held in place during use by weld(s) 62 (e.g., spot or seal welds
that can be
easily broken when it is desired to remove/replace the sleeve 52).
[0049] As those in the art should now appreciate, the general
installation
overview of FIGs. 5 and 5-1 also can be used for a capped thermal protective
sleeve
(with open or fused ends and a separate locating/securing cap at the proximal
end). As
such, the arrangement of FIG. 5 can be used for all lipped or capped sleeve
example
embodiments. This includes the radially ribbed, axially ribbed, the in-filled
lattice
sleeves of FIGs. 1A, 1B, 2A, 2B and so forth whether capped or lipped.
[0050] FIG. 6 illustrates capped thermal protective sleeves 70, 72 slip
fitted
within the bores of a flow device (e.g., the flanged input/output pipes of a
valve 74).
Like the lipped sleeve of FIG. 5, this arrangement applies in general to all
example
thermally insulating sleeves. The sleeves 70, 72 are fitted into the flow
device 74 just
like sleeves 50, 52 are fitted into the flow device 54. However, as depicted
in the
enlarged view at FIG. 5-1, since a separate securing cap 76 is now employed
(instead of
the integral lip 56 in FIG. 5), the securing cap 76 is held in place during
use by weld(s)
78 (e.g., spot or seal welds that can be easily broken) while the distal other
end of a
sleeve is located against a smaller diameter bore section at the opposite
distal end of the
flow device bore (with a sufficiently small clearance fit to prevent ingress
of thermally
conductive material during use). This arrangement holds for all capped or
lipped sleeve
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example embodiments. This includes the radially ribbed, axially ribbed, the in-
filled
lattice sleeves of FIGs. 1A, 1B, 2A, 2B and so forth whether capped or lipped.
[0051] FIG. 7 is a cut-away schematic isometric view of valve 74 in FIG.
6
showing sleeve 70 having its distal end butted to a smaller diameter distal
end 80 of
flow device bore 82 and trapped there by the larger diameter cap 76 within
larger
diameter proximal bore 84 by weld(s) 78.
[0052] To establish some measure of efficiency for an example embodiment,
a 3-
dimensional finite element analysis using a transient thermal technique was
conducted
for a ball valve having a flanged end connector inside diameter of 2.3 inches
and an
outside diameter of 4.5 inches, subjected to extreme temperature and pressure
cycles
between 400 C (752 F) and 14 MPa (2,030.5 psi) respectively. Three different
setups
were used: the flow device without any thermal protective device; the flow
device with
the internal surface that interacts with the axial flow path coated with
thermal and wear
resistant materials; and the flow device with a thermal protective sleeve as
shown in
FIGs. 5-6. The thermal protective sleeve was made of Inconel 718 by
conventional
3D printing processes.
[0053] Peak stress intensities in the end connectors was found to be
605A/Pa for
the flow device without any thermal protective technology, 511A/Pa for the
model with
the thermal and wear-resistant coatings and 259A/Pa for the model with a
thermal
protective sleeve of the type described herein. This translates to a design
life of 1,800
cycles, 2,900 cycles and 40,000 cycles respectively from fatigue design curves
using
fatigue analysis based on American Society of Mechanical Engineers (ASME)
criteria
(i.e., ASME 2015 Boiler & Pressure Vessel Code Section II Part D and Section
III A
were used for the fatigue analysis).
[0054] Preferably the thermally insulating sleeve is additively
manufactured
(e.g., by 3D printing), constructed of a suitable material for the serviced
application
(e.g., Inconel 718 or other austenitic nickel-chromium-based super-alloys,
high nickel
alloys and the like or ceramic and/or composite materials of various types
recognized
by those in the art as being suitable for certain severe service applications)
with an
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internal infill structural pattern creating internal voids which increase
thermal insulation
properties while yet remaining structurally adequate to serve as a thermal
insulating
flow device liner for the serviced application. Preferably the infill is sized
to maximize
strength (i.e., to support internal/external pressures to be experienced by
the sleeve)
while concurrently also minimizing heat transfer (i.e., from the inside to the
outside of
the sleeve). Multi-layer material could also be used if the sleeve is made
with wear-
resistant, corrosion-resistant, low thermal conductivity materials. When a 3D
printed
sleeve comes out of the printer, it is in a green state. Subsequently parts
can be
subjected to hot isostatic pressing (sometimes referred to as being "hipped")
and/or heat
treated to reduce porosity and increase mechanical properties respectively.
Based on
testing, all these three states are believed to work.
[0055] Depending on the application, the interior surface of the example
embodiments may be sprayed with a suitable wear-resistant coating as those in
the art
will appreciate.
[0056] The functionality of the example embodiments is not limited to any
particular flow device as those in the art will appreciate.
[0057] Example thermal insulating sleeve liners for a fluid flow device
provide a
loosely-fit additively manufactured thermal protective sleeve disposed axially
in bores
of flow devices such valves and pipes. The sleeve may have variable designs
depending on applications and may include, but are not limited to: (a) a
sleeve made of
an internal shell, an outer shell and an infill pattern; (b) a sleeve with
radial ridges; (c) a
sleeve that is ribbed axially ¨ and wherein the infill lattice structures and
exterior
surface patterns may be modified to meet process parameters. Any of these
examples
may be lipped or capped depending on the preferred arrangement and/or weld.
[0058] An example thermal insulating sleeve liner structure having an
internal
shell, an outer shell and fused ends may have an airtight vacuumed infill
chamber.
[0059] An example flow device fitted with an example thermal insulating
sleeve
liner may have an internal shell, an outer shell an infill chamber there-
between with
fused ends and a pressure equilibrium hole there-through.
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16
[0060] An example thermal insulating sleeve liner structure may have an
internal
shell, outer shell, a pressurized infill chamber and seal-welded ends.
[0061] An example thermal insulating sleeve liner structure may be made
of a
high nickel alloy.
[0062] An example thermal insulating sleeve liner structure may have a
wear-
resistant coating on its inner surface of an internal shell.
[0063] An example thermal insulating sleeve liner structure may use a
securing
cap which may or may not be of the same material as the body of the flow
device to
which it is welded within a bore of the flow device. Alternatively, the
securing cap
may be threaded for a threaded connection with the bore of a flow device.
[0064] An example thermal insulating sleeve liner structure may include
an
integral lip welded to a bore on the body of the protected flow device.
[0065] While the invention has been described in connection with what is
presently considered to be the most practical and preferred embodiments, it is
to be
understood that the invention is not to be limited to the disclosed
embodiments, but on
the contrary, is intended to cover various modifications and equivalent
arrangements
included within the spirit and scope of the appended claims.
